View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68336U 26145.29423242 +.00000000 +00000-0 +17927-3 0 00004
2 68336 53.1598 352.4859 0001047 71.4244 288.6870 15.30195623 03
| Epoch (UTC): | 25 May 2026 07:03:41 |
| Eccentricity: | 0.0001047 |
| inclination: | 53.1598° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 352.4859° |
| argument of perigee: | 71.4244° |
| revolutions per day: | 15.30195623 |
| mean anomaly at epoch: | 288.6870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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